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Last edited by ImportBot
September 14, 2008 | History

Bianca T. Anderson

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  • Cover of: Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825

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  • Cover of: Effects of wing sweep on in-flight boundary-layer transition  for a laminar flow wing at Mach numbers from 0.60 to 0.79

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  • Cover of: Overview of supersonic laminar flow control research on the F-16XL ships 1 and 2

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  • Cover of: Techniques used in the F-14 variable-sweep transition flight experiment

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September 14, 2008 Created by ImportBot Imported from Oregon Libraries MARC record